Design and Simulation of Landing Control Instruction Model of Certain Type Aircraft
Instruction steering, as a basic working mode, is widely used in flight control system of thirdgeneration fighters, it helps to alleviate the burden of pilot and to enhance pilots control effectiveness. The feasibility of adding such landing instruction steering system in certain type aircraft is analyzed against aircraft approaching and landing by pure contact flight. The control instruction models for glide line, reference line and glide speed are separately designed. The simulation of pilotaircraft closed loop system with full motion equation is conducted. And the results show that the control instruction model can achieve landing instruction steering of the aircraft.
Instruction steering landing control instruction model glide line reference line glide speed
Yingxiao Yu Yufei Wang
Department of Aviation Life-saving Aviation University of Air Force Changchun, China
国际会议
太原
英文
358-361
2011-02-26（万方平台首次上网日期，不代表论文的发表时间）